▸Orbital parameters

Orbit class	SSO
Inclination	97.9759°
Eccentricity	0.0021903
Period	95.5 min
Apogee	557 km
Perigee	527 km
Mean motion	15.08017383 rev/day
RAAN	204.4553°
Arg of perigee	232.4105°
Mean anomaly	127.5134°
B*	1.0938e-4
Rev at epoch	56,343

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 41394U 16020A 26188.22491005 .00001622 00000-0 10938-3 0 9993

2 41394 97.9759 204.4553 0021903 232.4105 127.5134 15.08017383563434

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2515",
  "OBJECT_ID": "2016-020A",
  "EPOCH": "2026-07-07T05:23:52.228+00:00",
  "MEAN_MOTION": 15.08017383,
  "ECCENTRICITY": 0.0021903,
  "INCLINATION": 97.9759,
  "RA_OF_ASC_NODE": 204.4553,
  "ARG_OF_PERICENTER": 232.4105,
  "MEAN_ANOMALY": 127.5134,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41394,
  "REV_AT_EPOCH": 56343,
  "BSTAR": 0.00010938,
  "MEAN_MOTION_DOT": 0.00001622,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	COSMOS 2515
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Mar 24, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3700HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/41394

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.